JPS6027826B2 - Vortex generation device for intake air-fuel mixture in internal combustion engine - Google Patents

Vortex generation device for intake air-fuel mixture in internal combustion engine

Info

Publication number
JPS6027826B2
JPS6027826B2 JP50119579A JP11957975A JPS6027826B2 JP S6027826 B2 JPS6027826 B2 JP S6027826B2 JP 50119579 A JP50119579 A JP 50119579A JP 11957975 A JP11957975 A JP 11957975A JP S6027826 B2 JPS6027826 B2 JP S6027826B2
Authority
JP
Japan
Prior art keywords
internal combustion
combustion engine
fuel mixture
vortex
intake air
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP50119579A
Other languages
Japanese (ja)
Other versions
JPS5243023A (en
Inventor
シヤク フ− オン
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP50119579A priority Critical patent/JPS6027826B2/en
Priority to CA262,168A priority patent/CA1090220A/en
Priority to GB40640/76A priority patent/GB1568243A/en
Priority to IT27854/76A priority patent/IT1077048B/en
Priority to SE7610826A priority patent/SE7610826L/en
Priority to NZ182206A priority patent/NZ182206A/en
Priority to AU18322/76A priority patent/AU515533B2/en
Priority to DE19762644444 priority patent/DE2644444A1/en
Priority to BR7606587A priority patent/BR7606587A/en
Priority to FR7629802A priority patent/FR2326587A1/en
Publication of JPS5243023A publication Critical patent/JPS5243023A/en
Priority to US06/172,693 priority patent/US4307697A/en
Publication of JPS6027826B2 publication Critical patent/JPS6027826B2/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M29/00Apparatus for re-atomising condensed fuel or homogenising fuel-air mixture
    • F02M29/04Apparatus for re-atomising condensed fuel or homogenising fuel-air mixture having screens, gratings, baffles or the like
    • F02M29/06Apparatus for re-atomising condensed fuel or homogenising fuel-air mixture having screens, gratings, baffles or the like generating whirling motion of mixture

Description

【発明の詳細な説明】 本発明は燃料供給手段として気化器あるいは燃料噴射装
置を用いた内燃機関における吸入混合気の供給装置に関
するものであって、特に吸入経路途中に複数系統の混合
気による渦流を生成させるようにした新規な吸入混合気
の供給装置に係るものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an intake mixture supply device for an internal combustion engine using a carburetor or a fuel injection device as a fuel supply means. This invention relates to a novel intake air-fuel mixture supply device that generates.

主としてガソリンエンジンにおける燃焼効率の向上の一
助として、吸入経路途中に案内羽根を設け、これによっ
て吸入する混合気に渦流を生じさせ、ガソリン粒子の均
一な混合及び粒子の微細化などを図ることが行われてい
る。
Mainly to help improve combustion efficiency in gasoline engines, guide vanes are installed in the middle of the intake path to create a vortex in the intake air-fuel mixture, thereby achieving uniform mixing of gasoline particles and miniaturization of the particles. It is being said.

しかしながら従来用いられている渦流生成装置は、第1
6図に示すように円環状をなす渦流生成装置1′におけ
る案内羽根を同一方向に偏向させた構造であって、この
装置によれば吸入経路内には第16図中矢印Aで示すよ
うな単純な一系統の渦流しか生じさせることができない
のである。しかもこのような渦流の場合には、旋回途中
で遠心力が生じ質量のあるガソリン粒子は均一に混合す
るどころか管壁内に押し付けられるようになって、管壁
側において混合気が濃くなり中心部は薄くなるという不
均一な混合状態となるものであり、所期の効果は上げら
れていないのが現状であった。換言すれば従来は少なく
とも禍流を生じせしめることが内燃機関の性能向上に寄
与することが知られているにとどまり、これを複数系統
とするという根本的な技術思想は未だ開示されていなか
ったのである。このような従釆手法の欠点を解消するた
めに本発明がなされたものであって、それによれば燃焼
室内に吸入混合気を供給するにあたり、複数系統を生成
させながら吸入混合気を供給し、より高率的なガソリン
粒子の均一化、微細化を図り完全燃焼を達成し炭化水素
や一酸化炭素等の有害排気ガス成分の減少を達成したも
のである。以下本発明を図示の実施例に基づいて具体的
に説明すると、第1図は本発明たる渦流生成装置を取り
付けた状態を示すものであって、気化器Cと吸気管1と
の間に本体1を設けるものである。
However, the conventionally used vortex generation device
As shown in Fig. 6, the guide vanes of the annular vortex generating device 1' are deflected in the same direction. It is only possible to generate one simple system of eddies. Moreover, in the case of such a vortex flow, centrifugal force occurs during swirling, and the heavy gasoline particles are not mixed uniformly, but are forced into the pipe wall, resulting in the mixture becoming thicker on the pipe wall side and concentrated in the center. This results in a non-uniform mixing state in which the mixture becomes thinner, and the desired effect has not been achieved at present. In other words, until now it was only known that generating at least a calamity flow contributed to improving the performance of an internal combustion engine, but the fundamental technical idea of creating multiple systems for this had not yet been disclosed. be. The present invention has been made in order to eliminate the drawbacks of such a secondary method, and according to the present invention, when supplying the intake mixture into the combustion chamber, the intake mixture is supplied while generating multiple systems, It achieves complete combustion by achieving a higher rate of homogenization and miniaturization of gasoline particles, and a reduction in harmful exhaust gas components such as hydrocarbons and carbon monoxide. Below, the present invention will be specifically explained based on the illustrated embodiments. FIG. 1.

尚、符号Eはエンジン本体を示すとともに前記気化器C
からエンジンEにおけるシリンダまでの間を吸入経路と
定義する。また本装置を適用するにあたっては、通常の
4サイクルガソリンエンジン、2サイクルガソリンエン
ジン、ロータリーエンジン等に適用できるものであり、
加えてこれら各種のエンジンに対する燃料供聯合手段に
ついても気化器によるもののほか燃料噴射方式のもので
あってもよい。この渦流生成装直1は全体として円環状
をなすものであって、その底部に一体的に複数の案内羽
根2を形成するものである。この案内羽根2は本体の一
部を曲成したものであって、それぞれ第3図から第6図
に示すように案内羽根2は羽根先を互いに離反させた一
対の案内羽根2からなる分離組a,a′と羽根先を互い
に向き合わせた一対の案内羽根からなる集合絹b,b′
及びそれら両者の間に設けられる補助案内羽根cとがあ
り、これらを適宜組み合わせて一つの装置として用いる
ものである。以下これらの種々の実施例を説明すると、
第7図から第10図に示す実施例は、断面円形の吸気管
1に対し渦流生成装置を付設する場合に適用するもので
ある。先ず第7図は一組の分離組a,a′と、一組の集
合線b,b′を設け、その間に補助案内羽根cを設ける
ようにしたものであり、これにより図中矢印Aで示す渦
流を2系統生成するものである。同じく第8図は4系統
、第9図は10系統、第10図は12系統の渦流Aを生
成するものである。尚、このうち第9図及び第10図に
示す実施例は分離組a,a′のみを多数組形成すること
によって渦流Aを生成しているものである。更に第11
図から第13図は断面楕円形の吸気管1に適用する実施
例を示すものであって、これ以外、角形断面形状等適宜
の断面形状を有する吸気管にも適用できるものである。
これら第11図から第13図は楕円形をなす吸気管1内
においてそれぞれ2系統、4系統、8系統の渦流を生成
するものである。尚、ここで例えば第13図に実線の円
○で囲む部分が分離組a,a′であるが、これを見方を
変えて破線の円○′で囲む案内羽根の組をみるとこれら
は正に集合組b,b′‘こほかならないものであり、こ
のように案内羽根2を接近して設けた場合には各案内羽
根がいずれの組をも構成するようにみえる場合が生ずが
、これらはいずれの組と呼称してもその作用の実態は変
わらないものである。更に第14図にはこの渦流生成装
置1における案内羽根を吸気管の管路方向にずらせて形
成した実施例を示すものであり、また第15図には渦流
生成装置を多段に構成した実施例を示すものである。勿
論この場合には、渦流生成装置を吸気管1と別部材とせ
ずに、吸気管1の内壁面あるいは気化器と吸気管との間
に設けられる断熱板(ヒートィンシュレータ)に形成し
てもよい。尚、このような第14図及び第15図に示さ
れている実施例では吸気の流れとともに混合気の渦流生
成が一層図られ、燃料粒子の相互の微細化がより達成で
き優れた燃焼状態を得ることができるものである。また
吸気管内に案内羽根2を設けるということは、これを吸
気弁に対しより近付けて設けることができるということ
を意味するものであり、このようにした時にはシリンダ
内でも複数系統の渦流がシリンダ軸線と直角方向にでき
ることなるのである。従ってシリンダ内での着火状態を
より良好なものとすることができるものである。このよ
うな具体的実施例によって、吸入混合気0が供給されて
いく途中で案内羽根2により旋回させられるようになる
ものであって、2系統以上の渦流中心軸が吸入経路の延
長方向に沿うような複数系統の渦流が形成されるもので
ある。
Incidentally, the symbol E indicates the engine body and the carburetor C.
The area between the engine E and the cylinder is defined as the intake path. In addition, when applying this device, it can be applied to ordinary 4-stroke gasoline engines, 2-stroke gasoline engines, rotary engines, etc.
In addition, the fuel supply means for these various engines may be of a fuel injection type in addition to a carburetor. The vortex generating device 1 has an annular shape as a whole, and a plurality of guide vanes 2 are integrally formed at the bottom thereof. This guide vane 2 is a part of the main body that is curved, and as shown in FIGS. 3 to 6, the guide vane 2 is a separated assembly consisting of a pair of guide vanes 2 whose vane tips are separated from each other. A set of silk b, b' consisting of a, a' and a pair of guide vanes with their blade tips facing each other
and an auxiliary guide vane c provided between them, and these are used in appropriate combination as one device. These various examples will be explained below.
The embodiments shown in FIGS. 7 to 10 are applied when a vortex generation device is attached to an intake pipe 1 having a circular cross section. First, in Fig. 7, a set of separated sets a, a' and a set of set lines b, b' are provided, and an auxiliary guide vane c is provided between them. It generates two systems of vortex flows as shown. Similarly, FIG. 8 shows four systems of eddy currents A, FIG. 9 shows 10 systems, and FIG. 10 generates 12 systems of vortex currents A. Incidentally, in the embodiment shown in FIGS. 9 and 10, the vortex A is generated by forming a large number of only separated sets a and a'. Furthermore, the 11th
13 shows an embodiment applied to an intake pipe 1 having an elliptical cross-section, but the present invention can also be applied to an intake pipe having an appropriate cross-sectional shape such as a rectangular cross-section.
11 to 13 show that two, four, and eight systems of vortex flow are generated in the elliptical intake pipe 1, respectively. Here, for example, in Fig. 13, the part surrounded by a solid circle ○ is the separated sets a and a', but if you look at it from a different perspective and look at the guide vane set surrounded by a broken line circle ○', these are correct. There is no other than the sets b and b'', and when the guide vanes 2 are disposed close to each other in this way, it may appear that each guide vane constitutes any set. No matter what group these are called, the actual state of their action remains the same. Furthermore, FIG. 14 shows an embodiment in which the guide vanes of this vortex generation device 1 are shifted in the direction of the intake pipe, and FIG. 15 shows an embodiment in which the vortex generation device is configured in multiple stages. This shows that. Of course, in this case, the vortex generating device is not formed as a separate member from the intake pipe 1, but is formed on the inner wall surface of the intake pipe 1 or on a heat insulator provided between the carburetor and the intake pipe. Good too. In the embodiment shown in FIGS. 14 and 15, the vortex of the air-fuel mixture is further generated along with the flow of intake air, and the mutual miniaturization of fuel particles is further achieved, resulting in an excellent combustion state. It is something that can be obtained. Furthermore, providing the guide vane 2 in the intake pipe means that it can be provided closer to the intake valve, and when this is done, multiple systems of vortex flow can flow along the cylinder axis. This can be done in a direction perpendicular to this. Therefore, the ignition condition within the cylinder can be improved. With such a specific embodiment, the intake air-fuel mixture 0 is made to swirl by the guide vane 2 while being supplied, and the center axes of the vortex flow of two or more systems are along the extension direction of the intake path. Multiple systems of vortex flows are formed.

このように本発明は根本的に内燃機関における吸入混合
気夕の供)給装置に新規な手法を案出したものであり、
吸気管内における複数系統の渦流により燃料の粒子が相
互に衝突し、より微細化が達成され、好ましい燃焼状態
を得るのである。
In this way, the present invention fundamentally devises a new method for the intake air-fuel mixture supply device in an internal combustion engine.
The multiple systems of vortex flow within the intake pipe cause fuel particles to collide with each other, achieving further refinement and achieving favorable combustion conditions.

【図面の簡単な説明】[Brief explanation of the drawing]

0 第1図は本発明たる渦流生成装置を内燃機関に組込
んだ状態を示す一部破断側面図、第2図は本装置の一実
施例を示す斜視図、第3図〜第6図は本装置の要素たる
案内羽根の各組合せ形態を示す平面図、第7図〜第13
図は本装置の各種の実施5例を示す平面図、第14図及
び第15図は更に他の実施例を示す縦断側面図、第16
図はこの種の装置の従来型を示す平面図である。 1…渦流生成装置、2・・・案内羽根、1…吸気管、A
…渦流、C・・・補助案内羽根、a,a′・・・案内0
羽根の分離組、b,b′・・・案内羽根の集合組。 第1図第2図 第3図 第4図 第5図 第6図 第7図 第9図 第8図 第10図 第11図 第12図 第13図 第15図 第14図 第16図
0 Fig. 1 is a partially cutaway side view showing the vortex generating device of the present invention installed in an internal combustion engine, Fig. 2 is a perspective view showing an embodiment of the device, and Figs. 3 to 6 are Plan views showing various combinations of guide vanes, which are elements of this device, FIGS. 7 to 13
The figure is a plan view showing five various embodiments of this device, FIGS. 14 and 15 are longitudinal sectional side views showing still other embodiments, and FIG.
The figure is a plan view showing a conventional type of device of this type. 1... Vortex generating device, 2... Guide vane, 1... Intake pipe, A
...vortex, C... auxiliary guide vane, a, a'... guide 0
Separate set of vanes, b, b'... set of guide vanes. Figure 1 Figure 2 Figure 3 Figure 4 Figure 5 Figure 6 Figure 7 Figure 9 Figure 8 Figure 10 Figure 11 Figure 12 Figure 13 Figure 15 Figure 14 Figure 16

Claims (1)

【特許請求の範囲】[Claims] 1 内燃機関の燃料混合気の供給経路途中に設けられる
環状の本体に対し、その一部を内側に曲成させて案内羽
根を形成して成り、この案内羽根は、互いに隣接する案
内羽根の先端を離反させるように形成した分離組と、互
いに隣接する案内羽根の先端を接近させるように形成し
た集合組とのいずれか一方又は双方を具えていることを
特徴とする内燃機関における吸入混合気渦流生成装置。
1 A guide vane is formed by bending a part of an annular body provided in the middle of the fuel mixture supply path of an internal combustion engine inward, and the guide vane is formed by the tips of the adjacent guide vanes. An intake air-fuel mixture vortex in an internal combustion engine characterized by comprising either one or both of a separating set formed to separate the guide vanes and a set set formed so that the tips of adjacent guide vanes approach each other. generator.
JP50119579A 1975-10-02 1975-10-02 Vortex generation device for intake air-fuel mixture in internal combustion engine Expired JPS6027826B2 (en)

Priority Applications (11)

Application Number Priority Date Filing Date Title
JP50119579A JPS6027826B2 (en) 1975-10-02 1975-10-02 Vortex generation device for intake air-fuel mixture in internal combustion engine
CA262,168A CA1090220A (en) 1975-10-02 1976-09-28 Complex swirl static mixer for engines
GB40640/76A GB1568243A (en) 1975-10-02 1976-09-30 Device for agitating an air-fuel mixture for an internal combustion engine
IT27854/76A IT1077048B (en) 1975-10-02 1976-09-30 STATIC MIXER DEVICE GENERATOR OF COMPLEX VORTICULOUS MOVEMENTS FOR INTERNAL COMBUSTION ENGINES
SE7610826A SE7610826L (en) 1975-10-02 1976-09-30 STATIC MIXER FOR AN COMBUSTION ENGINE
NZ182206A NZ182206A (en) 1975-10-02 1976-10-01 Static mixture which forms complex swirls in the air-fuel mixture of internal combustion engine
AU18322/76A AU515533B2 (en) 1975-10-02 1976-10-01 Device for swirling air-fuel mixture
DE19762644444 DE2644444A1 (en) 1975-10-02 1976-10-01 METHOD AND DEVICE FOR TURBILIZING AN AIR-FUEL MIXTURE IN AN INTERNAL COMBUSTION ENGINE
BR7606587A BR7606587A (en) 1975-10-02 1976-10-01 COMBUSTIBLE AIR MIXING PROCESS, STATIC TURBILLION MIXER AND INTERNAL COMBUSTION ENGINE
FR7629802A FR2326587A1 (en) 1975-10-02 1976-10-04 METHOD AND DEVICE FOR IMPROVING THE MIXING OF AIR CURRENT AND FUEL IN AN INTERNAL COMBUSTION ENGINE
US06/172,693 US4307697A (en) 1975-10-02 1980-07-28 Complex swirl static mixer for engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP50119579A JPS6027826B2 (en) 1975-10-02 1975-10-02 Vortex generation device for intake air-fuel mixture in internal combustion engine

Publications (2)

Publication Number Publication Date
JPS5243023A JPS5243023A (en) 1977-04-04
JPS6027826B2 true JPS6027826B2 (en) 1985-07-01

Family

ID=14764834

Family Applications (1)

Application Number Title Priority Date Filing Date
JP50119579A Expired JPS6027826B2 (en) 1975-10-02 1975-10-02 Vortex generation device for intake air-fuel mixture in internal combustion engine

Country Status (11)

Country Link
US (1) US4307697A (en)
JP (1) JPS6027826B2 (en)
AU (1) AU515533B2 (en)
BR (1) BR7606587A (en)
CA (1) CA1090220A (en)
DE (1) DE2644444A1 (en)
FR (1) FR2326587A1 (en)
GB (1) GB1568243A (en)
IT (1) IT1077048B (en)
NZ (1) NZ182206A (en)
SE (1) SE7610826L (en)

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Also Published As

Publication number Publication date
FR2326587A1 (en) 1977-04-29
SE7610826L (en) 1977-04-03
NZ182206A (en) 1979-11-01
FR2326587B1 (en) 1982-12-03
AU1832276A (en) 1978-04-06
IT1077048B (en) 1985-04-27
US4307697A (en) 1981-12-29
DE2644444A1 (en) 1977-04-14
GB1568243A (en) 1980-05-29
AU515533B2 (en) 1981-04-09
CA1090220A (en) 1980-11-25
JPS5243023A (en) 1977-04-04
BR7606587A (en) 1977-06-28

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